A Lunar-Orbiting Satellite Constellation for Wireless Energy Supply
The goal of this research is to define a lunar-orbiting system that provides power to the lunar surface through wireless power transmission. To meet the power demand of a lunar base, a constellation of satellites placed in stable orbits is used. Each satellite of this constellation consists of solar...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
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MDPI AG
2023-10-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/10/11/919 |
| _version_ | 1827641038692417536 |
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| author | Francesco Lopez Anna Mauro Stefano Mauro Giuseppe Monteleone Domenico Edoardo Sfasciamuro Andrea Villa |
| author_facet | Francesco Lopez Anna Mauro Stefano Mauro Giuseppe Monteleone Domenico Edoardo Sfasciamuro Andrea Villa |
| author_sort | Francesco Lopez |
| collection | DOAJ |
| description | The goal of this research is to define a lunar-orbiting system that provides power to the lunar surface through wireless power transmission. To meet the power demand of a lunar base, a constellation of satellites placed in stable orbits is used. Each satellite of this constellation consists of solar arrays and batteries that supply a power transmission system. This system is composed of a laser that transmits power to receivers on the lunar surface. The receivers are photonic power converters, photovoltaic cells optimized for the laser’s monochromatic light. The outputs of this work will cover the architecture of the system by studying different orbits, specifically analyzing some subsystems such as the laser, the battery pack and the receiver placed on the lunar ground. The study is conducted considering two different energy demands and thus two different receivers location: first, at the strategic location of the Artemis missions’ landing site, the Shackleton Crater near the lunar south pole; second, on the lunar equator, in anticipation of future and new explorations. The goal is to evaluate the possible configurations to satisfy the power required for a lunar base, estimated at approximately 100 kW. To do this, several cases were analyzed: three different orbits, one polar, one frozen and one equatorial (Earth–Moon distant retrograde orbit) with different numbers of satellites and different angles of the receiver’s cone of transmission. The main objective of this paper is to perform a comprehensive feasibility study of the aforementioned system, with specific emphasis placed on selected subsystems. While thermal control, laser targeting, and attitude control subsystems are briefly introduced and discussed, further investigation is required to delve deeper into these areas and gain a more comprehensive understanding of their implementation and performance within the system. |
| first_indexed | 2024-03-09T17:07:49Z |
| format | Article |
| id | doaj.art-d378d6e401e9473a93bdaea6f92fa923 |
| institution | Directory Open Access Journal |
| issn | 2226-4310 |
| language | English |
| last_indexed | 2024-03-09T17:07:49Z |
| publishDate | 2023-10-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Aerospace |
| spelling | doaj.art-d378d6e401e9473a93bdaea6f92fa9232023-11-24T14:22:42ZengMDPI AGAerospace2226-43102023-10-01101191910.3390/aerospace10110919A Lunar-Orbiting Satellite Constellation for Wireless Energy SupplyFrancesco Lopez0Anna Mauro1Stefano Mauro2Giuseppe Monteleone3Domenico Edoardo Sfasciamuro4Andrea Villa5Department of Mechanical and Aerospace Engineering, Politecnico di Torino, 10129 Torino, ItalyDepartment of Electronics and Telecommunications, Politecnico di Torino, 10129 Torino, ItalyDepartment of Mechanical and Aerospace Engineering, Politecnico di Torino, 10129 Torino, ItalyDepartment of Electronics and Telecommunications, Politecnico di Torino, 10129 Torino, ItalyDepartment of Mechanical and Aerospace Engineering, Politecnico di Torino, 10129 Torino, ItalyDepartment of Electronics and Telecommunications, Politecnico di Torino, 10129 Torino, ItalyThe goal of this research is to define a lunar-orbiting system that provides power to the lunar surface through wireless power transmission. To meet the power demand of a lunar base, a constellation of satellites placed in stable orbits is used. Each satellite of this constellation consists of solar arrays and batteries that supply a power transmission system. This system is composed of a laser that transmits power to receivers on the lunar surface. The receivers are photonic power converters, photovoltaic cells optimized for the laser’s monochromatic light. The outputs of this work will cover the architecture of the system by studying different orbits, specifically analyzing some subsystems such as the laser, the battery pack and the receiver placed on the lunar ground. The study is conducted considering two different energy demands and thus two different receivers location: first, at the strategic location of the Artemis missions’ landing site, the Shackleton Crater near the lunar south pole; second, on the lunar equator, in anticipation of future and new explorations. The goal is to evaluate the possible configurations to satisfy the power required for a lunar base, estimated at approximately 100 kW. To do this, several cases were analyzed: three different orbits, one polar, one frozen and one equatorial (Earth–Moon distant retrograde orbit) with different numbers of satellites and different angles of the receiver’s cone of transmission. The main objective of this paper is to perform a comprehensive feasibility study of the aforementioned system, with specific emphasis placed on selected subsystems. While thermal control, laser targeting, and attitude control subsystems are briefly introduced and discussed, further investigation is required to delve deeper into these areas and gain a more comprehensive understanding of their implementation and performance within the system.https://www.mdpi.com/2226-4310/10/11/919wireless power transmissionMoon energy supplylaserfrozen orbitEarth–Moon distant retrograde orbit |
| spellingShingle | Francesco Lopez Anna Mauro Stefano Mauro Giuseppe Monteleone Domenico Edoardo Sfasciamuro Andrea Villa A Lunar-Orbiting Satellite Constellation for Wireless Energy Supply Aerospace wireless power transmission Moon energy supply laser frozen orbit Earth–Moon distant retrograde orbit |
| title | A Lunar-Orbiting Satellite Constellation for Wireless Energy Supply |
| title_full | A Lunar-Orbiting Satellite Constellation for Wireless Energy Supply |
| title_fullStr | A Lunar-Orbiting Satellite Constellation for Wireless Energy Supply |
| title_full_unstemmed | A Lunar-Orbiting Satellite Constellation for Wireless Energy Supply |
| title_short | A Lunar-Orbiting Satellite Constellation for Wireless Energy Supply |
| title_sort | lunar orbiting satellite constellation for wireless energy supply |
| topic | wireless power transmission Moon energy supply laser frozen orbit Earth–Moon distant retrograde orbit |
| url | https://www.mdpi.com/2226-4310/10/11/919 |
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